The invention relates to a fighter, in particular to an airplane with a variable-angle wing. The airplane mainly comprises a landing gear, a machine body, a fixed wing and a movable wing, and is characterized in that the movable wing is arranged inside or outside the fixed wing, connecting rods which can be controlled to turn over are arranged in the front and at the rear part of the fixed wing and connected with a turnover device; chutes allowing bulges on the connecting rods to be clamped therein are formed in the movable wing. The movable wing hidden in the fixed wing can be driven by the connecting rods to leave the fixed wing and to be parallel to the fixed wing as long as the turnover device is operated to enable the connecting rods on the fixed wing to turn over, so that the original one fixed wing is changed into two wings (that is, the movable wing is added).
Airplane with variable-angle wing
2015-12-30
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Variable area wing developed for airplane
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Airplane wing leading edge variable camber flap
NTRS | 1980
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